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Basics of Fluid Mechanics, 2014a

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430 CHAPTER 11. COMPRESSIBLE FLOW ONE DIMENSIONAL<br />

Table -11.4.<br />

The Isothermal Flow basic parameters (continue)<br />

M<br />

4fL<br />

D<br />

P<br />

P ∗ P 0<br />

P 0<br />

∗<br />

ρ<br />

ρ ∗ T 0<br />

T 0<br />

∗<br />

0.75000 0.03095 1.1269 1.0255 1.1269 0.97344<br />

0.80000 0.00626 1.056 1.009 1.056 0.98700<br />

0.81000 0.00371 1.043 1.007 1.043 0.98982<br />

0.81879 0.00205 1.032 1.005 1.032 0.99232<br />

0.82758 0.000896 1.021 1.003 1.021 0.99485<br />

0.83637 0.000220 1.011 1.001 1.011 0.99741<br />

0.84515 0.0 1.000 1.000 1.000 1.000<br />

11.6.6 Isothermal Flow Examples<br />

There can be several kinds <strong>of</strong> questions aside from the pro<strong>of</strong> questions 18 . Generally,<br />

the “engineering” or practical questions can be divided into driving force (pressure<br />

difference), resistance (diameter, friction factor, friction coefficient, etc.), and mass<br />

flow rate questions. In this model no questions about shock (should) exist 19 .<br />

The driving force questions deal with what should be the pressure difference to<br />

obtain a certain flow rate. Here is an example.<br />

Example 11.15:<br />

A tube <strong>of</strong> 0.25 [m] diameter and 5000 [m] in length is attached to a pump. What<br />

should be the pump pressure so that a flow rate <strong>of</strong> 2 [kg/sec] will be achieved? Assume<br />

that friction factor f =0.005 and the exit pressure is 1[bar]. [ The ] specific heat for the<br />

gas, k =1.31, surroundings temperature 27 ◦ J<br />

C, R = 290<br />

Kkg<br />

. Hint: calculate the<br />

maximum flow rate and then check if this request is reasonable.<br />

Solution<br />

If the flow was incompressible then for known density, ρ, the velocity can be calculated<br />

by utilizing ΔP = 4 f̷L U 2<br />

D 2g . In incompressible flow, the density is a function <strong>of</strong> the<br />

entrance Mach number. The exit Mach number is not necessarily 1/ √ k i.e. the flow is<br />

not choked. First, check whether flow is choked (or even possible).<br />

18 The pro<strong>of</strong> questions are questions that ask for pro<strong>of</strong> or for finding a mathematical identity (normally<br />

good for mathematicians and study <strong>of</strong> perturbation methods). These questions or examples will appear<br />

in the later versions.<br />

19 Those who are mathematically inclined can include these kinds <strong>of</strong> questions but there are no real<br />

world applications to isothermal model with shock.

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